Numerical simulations of leading-edge vortex core axial velocity for flow over delta wings

DOI10.1007/S11431-009-0082-8zbMath1422.76052OpenAlexW2061367693MaRDI QIDQ1045449

Lan Chen, Jin-Jun Wang

Publication date: 15 December 2009

Published in: Science in China. Series E (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/s11431-009-0082-8

zbMATH Keywords

low Reynolds numbervortex flowsdelta wing

Mathematics Subject Classification ID

Viscous vortex flows (76D17)

Related Items (1)

Effect of wing planform on leading-edge vortex structures

Uses Software

• Spalart-Allmaras

Cites Work

• Approximate Riemann solvers, parameter vectors, and difference schemes
• High-resolution upwind schemes for the three-dimensional incompressible Navier-Stokes equations

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